View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 63955U 26145.26547980 +.00000000 +00000-0 +50104-3 0 00003
2 63955 43.0010 104.1078 0001095 262.7567 97.3160 15.27590940 07
| Epoch (UTC): | 25 May 2026 06:22:17 |
| Eccentricity: | 0.0001095 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 104.1078° |
| argument of perigee: | 262.7567° |
| revolutions per day: | 15.27590940 |
| mean anomaly at epoch: | 97.3160° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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